Gravity gradiometer

ABSTRACT

A gravity gradiometer is disclosed which has a pair of sensor bars  41, 42  mounted in housings  43  and  45 . Transducers  71  are located adjacent the bars for measuring movement of the bars in response to the gravity gradient tensor. Signals from the transducers are supplied to a SQUID device  367  for processing the signals. A connector is supplied for connecting the circuitry to external equipment which comprises a container  560  having a feed through filter  564 , a three terminal cap  565 , a relay  566  and an output terminal. The output terminal is connected to further RF attenuation which comprises a second connector  5   b  having parallel inductors and resistors.

FIELD OF THE INVENTION

This invention relates to a gravity gradiometer, and in particular, butnot exclusively, to a gravity gradiometer for airborne use. Theinvention has particular application for measuring diagonal andoff-diagonal components of the gravitational gradient tensor.

BACKGROUND OF THE INVENTION

A gravity gradiometer is disclosed in our International PatentApplication No. PCT/AU2006/001269 and several concurrently filedapplications. The content of International Patent Application No.PCT/AU2006/001269 is incorporated into this specification by thisreference.

Gravimeters are widely used in geological exploration to measure thefirst derivatives of the earth's gravitational field. Whilst someadvances have been made in developing gravimeters which can measure thefirst derivatives of the earth's gravitational field because of thedifficulty in distinguishing spatial variations of the field fromtemporal fluctuations of accelerations of a moving vehicle, thesemeasurements can usually be made to sufficient precision for usefulexploration only with land-based stationary instruments.

Gravity gradiometers (as distinct from gravimeters) are used to measurethe second derivative of the gravitational field and use a sensor whichis required to measure the differences between gravitational forces downto one part in 10¹² of normal gravity.

Typically such devices have been used to attempt to locate deposits suchas ore deposits including iron ore and geological structures bearinghydrocarbons.

The above-mentioned gradiometer has a sensor in the form of a sensormass which is pivotally mounted for movement in response to the gravitygradient.

Gravity gradiometers of the type described in the above Internationalapplications have super-conducting components which are housed in avacuum canister which in turn is located in a Dewar. The componentryincludes SQUID devices and other circuitry and in order to providesignals to external measuring equipment outside the Dewar, andconnectors are provided to connect internal wiring within the Dewar tothat equipment. Because of the super-conducting nature of the circuitry,the internal circuitry must be protected from RF interference fromoutside sources, such as telephone and television signals, etc. whichresult in currents passing from the external circuitry into the internalsuper-conducting circuitry which can result in incorrect measurementsbeing made or significant noise in the measurement signals.

SUMMARY OF THE INVENTION

The object of the invention is to provide a gravity gradiometer in whichthe internal super-conducting circuitry of the gradiometer is protectedfrom RF interference produced by outside sources.

The invention provides a gravity gradiometer for measuring components ofthe gravity gradient tensor, comprising:

a sensor for measuring the components of the gravity gradient tensor,the sensor including super-conducting componentry;

a Dewar in which the sensor is arranged;

a connector for connecting the super-conducting componentry within theDewar to external equipment outside of the Dewar, the connectorcomprising:

-   -   a container attached to the Dewar;    -   a feed through filter in the container for connection to a lead        within the Dewar;    -   a three terminal cap electrically connected to the feed through        filter;    -   a relay electrically connected to the three terminal cap; and    -   an output terminal on the container for connecting the relay to        an external lead.

Thus, the super-conducting componentry within the Dewar is protectedfrom RF interference by the relay, which needs to be closed in order toenable signals to be passed through the connector and also by the threeterminal cap and feed through filter, thereby preventing, or at leastsubstantially reducing, any RF interference which passes from leadsexternal of the Dewar to super-conducting componentry within the Dewar.

Preferably the feed through filter comprises an indicator connected inparallel to a load, the other side of the load being earthed. The loadmay be a capacitor or a resistor or the like.

Preferably the feed through filter comprises an inductor connected inparallel to one side of a capacitor, the other side of the capacitorbeing earthed.

Preferably the three terminal cap comprises a pair of inductors betweenwhich a capacitor is connected on one side, the capacitor beingconnected to earth on the other side.

Preferably the relay comprises a relay coil, a relay switch which isclosed when the relay coil is energised to enable signals from the threeterminal cap to pass to the terminal.

Preferably a current source is provided for supplying current to therelay coil when measurements are taken to energise the coil and closethe relay.

Preferably the three terminal cap is mounted on a first baffle locatedwithin the container and the relay is mounted on a second bafflecontained within the container.

Preferably the gradiometer has a second connector electrically connectedto the first connector, the second connector having a further RFattenuator comprising coils connected in parallel to the respectiveloads.

The loads in this embodiment are resistors.

BRIEF DESCRIPTION OF THE DRAWINGS

Preferred embodiments of the invention would be described, by way ofexample, with reference to the accompanying drawings, in which:

FIG. 1 is a schematic view of a gradiometer of one embodiment of theinvention.

FIG. 2 is a perspective view of a first mount forming part of a mountingof the gradiometer of the preferred embodiment;

FIG. 3 is a view of a second mount of the mounting;

FIG. 4 is a view from underneath the mount of FIG. 3;

FIG. 5 is a cross-sectional view along the line IV-IV of FIG. 3;

FIG. 6 is a cross-sectional view along the line V-V of FIG. 3;

FIG. 7 is a view of the assembled structure;

FIG. 8 is a view showing the sensor mounted on the gimbal structure;

FIG. 9 is a plan view of a bar of the preferred embodiment;

FIG. 10 is a diagram showing actuator control;

FIG. 11 is a block diagram showing operation of the rotatable supportsystem;

FIG. 12 is a view of a gradiometer of the preferred embodiment;

FIG. 13 is a view of a first mount of a second embodiment;

FIG. 14 is a view of part of the mounting of FIG. 13 to illustrate thelocation and extent of the flexural web of the first mount;

FIG. 15 is a view of the mounting of FIG. 13 from beneath;

FIG. 16 is a view of the mounting of FIG. 13 including a second mount ofthe second embodiment;

FIG. 17 is a cross-sectional view through the assembly shown in FIG. 16;

FIG. 18 is a view from beneath of the section shown in FIG. 17;

FIG. 19 is a view from beneath of the second mount of the secondembodiment;

FIG. 20 is a view of the second mount of FIG. 19 from above;

FIG. 21 is an exploded view of the second mount of the secondembodiment;

FIG. 22 is view of the assembled mounting and sensors according to thesecond embodiment;

FIG. 23 is a perspective view of the gradiometer with some of the outervacuum container removed;

FIG. 24 is a plan view of a housing for supporting a bar according to afurther embodiment of the invention;

FIG. 25 is an exploded view of part of the embodiment of FIG. 24;

FIG. 26 is a more detailed view of part of the housing of FIG. 24;

FIG. 27 is a circuit diagram of a transducer used in the preferredembodiment of the invention;

FIG. 28 is a side view of the physical layout of the transducer of thepreferred embodiment;

FIGS. 29, 30, 30A, 31, 32 and 33 are a series of diagrams showing theformation of the transducer of the preferred embodiment of theinvention;

FIG. 34 is a view similar to FIG. 26 but showing the transducer inplace;

FIG. 34A is a view of a more preferred embodiment of the coilarrangement shown in FIGS. 29 to 33;

FIG. 34B is a detailed view of part of the arrangement shown in FIG.34A;

FIG. 35 is a diagram to assist explanation of the circuits of FIGS. 36and 37;

FIG. 36 is a circuit diagram relating to the preferred embodiment of theinvention, particularly showing use of one of the sensors as an angularaccelerometer;

FIG. 37 is a frequency tuning circuit;

FIG. 38 is a diagram illustrating balancing of the sensors of thegradiometer of the preferred embodiment;

FIG. 39 is a circuit diagram of a calibration sensor used when balancingthe gradiometer;

FIG. 40 is a detailed view of the part of FIG. 24 circled and marked A;

FIG. 41 is a drawing of a connector used in the preferred embodiments ofthe invention;

FIG. 42 is a circuit diagram of the connector of FIG. 41;

FIG. 42A is a circuit diagram used with the circuit of FIG. 42;

FIG. 43 is a diagram of a sensor bar and transducer configuration of oneembodiment of the invention;

FIG. 44 is a circuit diagram of the configuration shown in FIG. 43;

FIG. 45 is a diagram illustrating a heat switch of one embodiment of theinvention;

FIG. 45A is a view of a housing part of the gradiometer according to oneembodiment;

FIG. 45B is a detailed view of part of the embodiment of FIG. 45A;

FIG. 45C is a cross-sectional view along the line 45C-45C of FIG. 45A;

FIG. 45D is a detailed view of part of the arrangement shown in FIG. 45Cfrom beneath;

FIG. 45E is a cross-section view along the line 45E-45E of FIG. 45D; and

FIG. 46 is a schematic diagram of a gradiometer according to oneembodiment of the invention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

FIG. 1 is a schematic view of a gravity gradiometer according to oneembodiment of the invention.

The gradiometer shown in FIG. 1 comprises a double walled Dewar 1 whichis supported in an external platform 2. The external platform 2 enablesadjustment of the Dewar and therefore the contents of the Dewar aboutthree orthogonal axes. The external platform 2 is generally known andits adjustment by suitable motors or the like is also known. Thus, adetailed description will not be provided.

A vacuum canister 3 is provided in the Dewar and the Dewar is suppliedwith liquid gas such as liquid helium He so that the gradiometer canoperate at cryogenic temperature. The Dewar 1 is closed by an end plate4 which includes connectors 5 a for connecting electrical leads (notshown) to external components (not shown).

The canister 3 is closed by an end plate 9 which includes connectors 5 bfor connecting electric leads (not shown) to the connectors 5 a. Thegradiometer has a main casing 61 formed from a twelve-sided ring 62 andhemispherical domes 63 (see FIG. 12). An internal mounting 5 isconnected to the ring 62. The ring 62 carries a support 65 to which afeed through flange 9 is coupled. A neck plug 11 formed of baffles 11 awhich sandwich foam 11 b is provided above the canister 3. The baffles11 a are supported on a hollow rod 93 which extends to the canister 3and which is also used to evacuate the canister 3.

With reference to FIG. 2 a first mount 10 of a rotatable mounting 5(FIG. 7) of the gradiometer is shown which comprises a base 12 and anupstanding peripheral wall 14. The peripheral wall 14 has a plurality ofcut-outs 16. The base 12 supports a hub 18.

FIGS. 3 and 4 show a second mount 20 which comprises a peripheral wall22 and a top wall 24. The peripheral wall 22 has four lugs 13 forconnecting the mount to the casing 61. The top wall 24 and theperipheral wall 22 define an opening 28. The peripheral wall 22 has afirst part 25, a second part 26 and a third part 27. The second mount 20is a monolithic integral structure and the first part 25 is formed bymaking a circumferential cut 19 through the peripheral wall except forthe formation of flexure webs as will be described hereinafter. Thethird part 27 is formed by making a second circumferential cut 29through the peripheral wall 22 except for flexure webs which will alsobe described hereinafter. The second mount 20 is mounted on the firstmount 10 by locating the hub 18 into the opening 28 and the lugs 13through respective cut-outs 16 as is shown in FIG. 7.

The first mount 10 is joined to the second mount 20. The first flexureweb 31 is formed in the first mount 10 so a primary mount portion of themount 10 can pivot about the web 31 relative to a secondary mountportion of the mount 10. This will be described in more detail withreference to the second embodiment shown in FIGS. 13 to 21.

The lugs 13 connect the mounting 5 in the canister 3 which, in turn,locates in the Dewar 1 for cryogenic operation of the gradiometer.

The Dewar is in turn mounted in a first external platform for courserotational control of the gradiometer about three orthogonal x, y, zaxes. The mounting 5 mounts the sensor 40 (which will be described inmore detail hereinafter and which is preferably in the form of a massquadrupole) for much finer rotational adjustment about the x, y and zaxes for stabilising the gradiometer during the taking of measurementsparticularly when the gradiometer is airborne.

The first flexure web 31 allows the first mount 10 to move relative tothe second mount 20 about a z axis shown in FIG. 7.

FIGS. 5 and 6 are views along the lines IV and V respectively which inturn are along the cuts 19 and 29 shown in FIG. 3. The peripheral wall22 may be cut by any suitable cutting instrument such as a wire cutteror the like. FIG. 5 shows the bottom surface 19 a formed by the cut 27.As is apparent from FIGS. 3 and 5 the cut 27 has two inverted v-shapedpeaks 34. The apex of the peaks 34 is not cut and therefore form asecond flexure web 33 which join the first part 25 to the second part26. Thus, the second part 26 is able to pivotally rotate relative to thefirst part 25 about the x axis in FIG. 7. The second cut 29 is shown inFIG. 6 and again the bottom surface 29 a formed by the cut 29 isvisible. Again the second cut 29 forms two v-shaped peaks 35 and theapexes of the peaks 35 are not cut and therefore form a third flexureweb 37 which connect the second part 26 to the third part 27. Thus, thethird part 27 is able to pivotal rotate about the y axis shown in FIG.7.

FIG. 8 shows sensor 40 mounted on the mounting. The sensor 40 is anOrthogonal Quadrupole Responder—OQR sensor formed of a first mass and asecond mass in the form of a first bar 41 and a second bar 42 (not shownin FIG. 8) orthogonal to the bar 41 and which is of the same shape asthe bar 41.

The bar 41 is formed in a first housing 45 and the bar 42 is formed in asecond housing 47. The bar 41 and housing 45 is the same as bar 42 andthe housing 47 except that one is rotated 90° with respect to the otherso that the bars are orthogonal. Hence only the housing 45 will bedescribed.

The housing 45 has an end wall 51 and a peripheral side wall 52 a. Theend wall 51 is connected to rim 75 (FIGS. 2 and 7) of the wall 14 of thefirst mount 10 by screws or the like (not shown). The bar 41 is formedby a cut 57 in the wall 51 except for a fourth flexure web 59 whichjoins the bar 41 to the wall 51. The flexure web is shown enlarged inthe top view of the bar 41 in FIG. 9. Thus, the bar 41 is able to pivotrelative to the housing 45 in response to changes in the gravitationalfield. The bar 42 is mounted in the same way as mentioned above and alsocan pivot relative to its housing 47 in response to changes in thegravitational field about a fifth flexure web 59. The housing 47 isconnected to base 12 (FIG. 2) of the first mount 10.

The bar 41 and the housing 45 together with the flexure web 59 in thisembodiment are an integral monolithic structure. However, the web 59 canbe made separate to the housing 45 and connected to the housing 45 andbar 41, as will be described in the embodiment of FIGS. 24 and 25

Transducers 71 (not shown in FIGS. 2 to 6) are provided for measuringthe movement of the bars and for producing output signals indicative ofthe amount of movement and therefore of the measurement of thedifferences in the gravitational field sensed by the bars.

FIG. 10 is a schematic block diagram showing actuator control tostabilise the gradiometer by rotating the mounting 5 about threeorthogonal axes (x, y, z). A controller 50 which may be a computer,microprocessor or the like outputs signals to actuators 52, 53, 54 and55. The actuator 52 could rotate the mounting 5 about the x axis, theactuator 54 could rotate the mounting 5 about the y axis and theactuator 54 could rotate the mounting 5 about the z axis. However, inthe preferred embodiment, two of the four actuators 52, 53, 54 and 55are used to rotate the mounting about each axis so that rotation abouteach axis is caused by a combination of two linear movements providedfrom two actuators. The linear movement provided by each actuator willbe described with reference to FIGS. 31 and 32. The position of themounting 5 is monitored so that appropriate feedback can be provided tothe controller 50 and the appropriate control signals provided to theactuators to rotate the support 10 as is required to stabilise thesupport during movement through the air either within or towed behind anaircraft.

The preferred embodiment also includes angular accelerometers which aresimilar in shape to the bars 41 and 42 but the shape is adjusted forzero quadrupole moment. The linear accelerometers are simple pendulousdevices with a single micro pivot acting as the flexural hinge.

FIG. 11 is a view of a feedback control used in the preferredembodiment.

FIG. 12 is a cut away view of the gradiometer ready for mounting in theDewar 1 for cryogenic operation which in turn is to be mounted in theexternal platform. Although FIGS. 2 to 8 show the gradiometer with thebars 41 and 42 top and bottom, the instrument is actually turned on itsside (90°) so that the bars 41 and 42 are at the ends as is shown inFIG. 12.

FIG. 12 shows the mounting 5 arranged within the casing 61 and formed bythe ring 62 and the transparent hemispherical ends 63. The ring 22 hasconnectors 69 for connecting the internal wiring from transducers 71(see FIG. 8) and SQUID (Superconducting Quantum Interference Device)Electronics located in the casing 61 to the connectors 5 b (FIG. 1).

The transducers 71 measure the angle of displacement of the bars 41 and42 and the control circuitry (not shown) is configured to measure thedifference between them.

Error correction can be performed numerically based on digitised signalsfrom the accelerometers and a temperature sensor.

The transducers 71 are SQuID based transducers and the error correctionis made possibly by the large dynamic range and linearity of the SQuIDbased transducers.

FIGS. 13 to 21 show a second embodiment in which like parts indicatelike components to those previously described.

In this embodiment the first mount 10 has cut-outs 80 which effectivelyform slots for receiving lugs (not shown) which are connected to themount 10 in the cut-outs 80 and also to the second mount 20 shown inFIGS. 19 to 21. In this embodiment the lugs are separate components sothat they can be made smaller, and more easily, made than being cut withthe second mount section 20 which forms the second flexure web 33 andthe third flexure web 37.

In FIG. 13 a cut 87 is made to define the part 18 a of the hub 18. Thecut 87 then extends radially inwardly at 88 and then around centralsection 18 c as shown by cut 101. The cut 101 then enters into thecentral section 18 c along cut lines 18 d and 18 e to define a core 18f. The core 18 f is connected to the central section 18 c by theflexural web 31 which is an uncut part between the cut lines 18 e and 18d. The part 10 a therefore forms a primary mount portion of the mount 10which is separated from a secondary mount portion 10 a of the mount 10except for where the portion 18 a joins the portion 10 a by the flexuralweb 31. The part 18 a effectively forms an axle to allow for rotation ofthe part 18 a relative to the part 10 a in the z direction about theflexure web 31.

As is shown in FIG. 14, the cut line 88 tapers outwardly from the upperend shown in FIG. 14 to the lower end and the core 18 c tapers outwardlyin corresponding shape, as best shown in FIG. 17.

As is apparent from FIGS. 13 to 18, the first mount 10 is octagonal inshape rather than round, as in the previous embodiment.

FIGS. 19 to 21 show the second mount 20. FIG. 16 shows the second mount20 mounted in the first mount 10. As is best shown in FIGS. 19 and 20,the second mount 20 has cut-outs 120 which register with the cut-outs 80for receiving lugs (not shown). The lugs can bolt to the second mount 20by bolts which pass through the lugs and into bolt holes 121. The lugs(not shown) are mounted to the mount 20 before the mount 20 is securedto the first mount 10.

In the embodiment of FIGS. 19 and 20, the peaks 34 and inverted peaks 35are flattened rather than of V-shape as in the previous embodiment.

In this embodiment, top wall 24 is provided with a central hole 137 andtwo attachment holes 138 a. Three smaller holes 139 a are provided tofacilitate pushing of the housing 45 off the part 18 a if disassembly isrequired. When the second mount 20 is located within the first mount 10,the upper part of central section 18 c projects through the hole 137, asbest shown in FIG. 16. The mount 20 can then be connected to the mount10 by fasteners which pass through the holes 138 and engage in holes 139b (see FIG. 13) in the part 18 a.

Thus, when the first housing 45 and its associated bar 41 is connectedto the rim 75 of the housing 10 and the second housing 47 is connectedto the base 12, the housings 45 and 47 and their associated bars 41 and42 are therefore able to move about three orthogonal axes defined by theflexure web 31, the flexure web 33 and the flexure web 37.

As is best seen in FIG. 21 which is an exploded view of the three parts25, 26 and 27 which make up the second mount 20, an opening extendsthrough the mount 20 which is formed by the hole 137, hole 138 and hole139. It should be understood that the mount 20 shown in FIG. 21 is amonolithic structure and is merely shown in exploded view to clearlyillustrate the location of the flexural webs 33 and 35. Obviously theflexural web 33 shown in FIG. 21 joins with the part 26 and the flexuralweb 35 shown in FIG. 21 joins with the part 27. The holes 137, 138 and139 define a passage through which the axle or first portion 18 a of thefirst mount 10 can extend when the second mount 20 is located in thefirst mount 10.

Thus, when the second mount 20 is fixed to the part 18 a, the secondmount 20 can pivot with the first portion 10 a of the first mount 10about a z axis defined by the flexure web 31 whilst the second portionformed by the part 18 a remains stationary. Movement about the x and yaxes is achieved by pivotal movement of the second mount 20 about theflexure webs 33 and 35 as previously described.

FIG. 22 shows the linear and annular accelerometers 90 fixed to thehousings 45 and 47.

The gravity gradient exerts a torque on a rigid body with any massdistribution provided it has a non-zero quadrupole moment. For a planarbody, in the x-y plane and pivoted about the z-axis, the quadrupole isthe difference between moments of inertia in the x and y directions.Thus a square or circle has zero quadrupole moment, while a rectanglehas a non-zero value.

The torque produced is what constitutes the signal measured by thegradiometer.

There are two dynamical disturbances which can also produce torques andconsequently are sources of error.

The first is linear acceleration.

This produces a torque if the center of mass is not exactly at thecenter of rotation—i.e. the bar is “unbalanced”. The bars 41 and 42 arebalanced as well as possible (using grub screws to adjust the positionof the center of mass) but this is not quite good enough, so there is aresidual error. This error can be corrected by measuring the linearacceleration and using this to numerically subtract away the erroneouspart of the signal.

The second is angular motion.

There are two aspects to angular motion, each of which produces adifferent error.

The first is aspect angular acceleration.

Angular acceleration produces a torque on the mass distribution throughits moment of inertia (even if the quadrupole moment is zero). This isan enormous error and two preferred techniques are used to counteractit.

The first is to use internal rotational stabilization. This is depictedin the block diagram of FIG. 10. Here Ho(s) represents the sensorassembly pivoted about the mounting 5 (as per FIG. 9). The block A(s)represents the actuator, which provides the feedback torque to effectthe stabilization by canceling the applied disturbances. T(s) representsthe sensor (or transducer) which measures the effect of the applieddisturbance. This is the angular accelerometer. Using angularaccelerometers in rotational control is unusual—usually gyros and/orhighly damped tilt meters are used, but for our purpose the angularaccelerometers are better, as the error is proportional to the angularacceleration disturbance.

The second is to use common mode rejection CMRR—that is why 2 orthogonalbars are needed. For the two bars, the error torque produced by theangular acceleration is in the same direction, but the signal torqueproduced by the gravity gradient is in opposite direction.

Therefore, by measuring the difference in deflection between the twobars, the gradient is sensed but not the angular acceleration.

Therefore, two separate angular accelerometers 90 (labeled 90′ in FIG.22 for ease of identification) are provided. We have two independentoutput signals from the pair of OQR bars 41 and 42. The first isproportional to the difference in deflection, which gives the gradientsignal and the second is proportional to the sum of their deflections,which is proportional to the angular acceleration and provides thesensor for the z-axis rotational control.

The x and y axes require separate angular accelerometers. Rotationalstabilization about these axes is required because the pivot axes of thetwo bars are not exactly parallel and also to counteract the second formof error produced by angular disturbance, discussed below.

The second aspect is angular velocity.

Angular velocity produces centrifugal forces, which are also a source oferror. The internal rotational stabilization provided by the actuatorsreduces the angular motion so that the error is below 1 Eotvos.

FIG. 23 shows main body 61 and connector 69 with the hemispherical endsremoved.

FIG. 24 is a plan view of housing 45 according to a still furtherembodiment of the invention. As is apparent from FIG. 24, the housing 45is circular rather than octagonal, as is the case with the embodiment ofFIG. 8.

The housing 45 supports bar 41 in the same manner as described viaflexure web 59 which is located at the center of mass of the bar 41. Thebar 41 is of chevron shape, although the chevron shape is slightlydifferent to that in the earlier embodiments and has a more rounded edge41 e opposite flexure web 59 and a trough-shaped wall section 41 f, 41 gand 41 h adjacent the flexure web 59. The ends of the bar 41 havescrew-threaded bores 300 which receive screw-threaded members 301 whichmay be in the form of plugs such as grub screws or the like. The bores300 register with holes 302 in the peripheral wall 52 a of the housing45. The holes 302 enable access to the plugs 301 by a screwdriver orother tool so that the plugs 301 can be screwed into and out of the bore300 to adjust their position in the bore to balance the mass 41 so thecenter of gravity is at the flexure web 59.

As drawn in FIG. 24, the bores 300 are a 45° angle to the horizontal andvertical in FIG. 24. Thus, the two bores 302 shown in FIG. 24 are atright angles with respect to one another.

FIG. 24 also shows openings 305 for receiving the transducer 71 formonitoring the movement of the bar 41 and producing signals which areconveyed to the SQUID device. Typically, the transducer is in the formof a coil and as the bar 41 moves slightly due to the gravity differenceat ends of the bar, a change in capacitance occurs which alters thecurrent in the coil to thereby provide a signal indicative of movementof the bar 41.

In the embodiment of FIG. 24, the flexure web 59 is not integral withthe bar 41 and housing 45 but is rather formed on a separate web element501.

In this embodiment the bar 41 (and also the bar 42 in the secondhousing, not shown in FIGS. 24 and 25) are cut separate to the housing45. The bar 41 is formed with a dove-tail shaped channel 502 and thehousing 45 is provided with a correspondingly shaped dove-tail channel503.

As is best shown in FIG. 25, the web element 501 is of double dove-tailshape having a first dove-tail part 501 a and a second dove-tail part501 b which are joined together by the flexure web 59. The parts 501 and501 b are separated by a cut 504 apart from the location of the flexureweb 59.

The part 501 a is shaped and configured to fit into the channel 503 andthe part 501 b is shaped and configured to fit into the channel 502.Thus, when the element 501 is located into the channels 502 and 503, theelement 501 joins the bar 41 to the housing 45 and provides the flexureweb 59 to enable movement of the bar 41 in the housing 45.

In order to secure the element 501 in the channels 502 and 503, theelement 501 is cooled to a low temperature so that it effectivelyshrinks relative to its ambient temperature size. The housing 45 and thebar 41 can be heated so that they expand to increase the size of thechannels 502 and 503 relative to their ambient temperature state. Thus,the shrunk element 501 can easily fit into the channels 502 and 503 as arelatively snug fit and when both the element 501 and the bar 41 andhousing 45 return to ambient temperature, the housing 41 and bar 45effectively contract or shrink relative to the element 501 which expandsthereby causing the element 501 to tightly lock in the channels 502 and503.

When the gradiometer is used at cryogenic temperatures, both the element501 and the bar and housing will experience the same temperature, andtherefore temperature difference between that which occurred when theelement 501 was fitted into the channels 502 and 503 is maintained tomaintain the lock and integrity of the connection of the element 501 tothe bar 41 and housing 45.

The use of the element 501 means that the flexure web 59 is formed on aseparate component and if the web 59 breaks, the element 501 can simplybe removed and replaced by a new element. This therefore avoids the needto replace the entire housing 45 and bar 41 in the event that theflexure web 59 does break.

The flexure webs 31, 33 and 37 could be formed on separate web elementssimilar to the element 501 instead of being integral with theirrespective mounting parts to thereby avoid the need to replace theentire mounting part, should one of those webs break.

FIG. 26 is a more detailed view of part of the housing of FIG. 24showing the openings 305. As can be seen from FIG. 25, the openings 305have shoulders 401 which form grooves 402. A spring 403 is arrangedadjacent surface 406.

FIGS. 27 to 33 are drawings relating to the transducer 71 used in thepreferred embodiments of the invention, which measure the movement ofthe bars 41 and 42 in the housings 45 and 47. Only one of thetransducers is shown in FIGS. 27 to 33.

As is shown in FIG. 27 the transducer 70 has two sensing coils 510 and511 which have their inductance modulated by the motion ofsuperconducting surface 41 a of the bar 41, as the bar 41 moves aboutthe flexure web 59 in response to changes in the gravitational field.The coil 510 is a large inductance fine pitch coil with many turns whichis intended to carry a relatively low current. The coil 511 is a lowinductance coarse pitch pancake coil with fewer turns and is tightlycoupled to coil 510 but separated from the coil 510 by a thin insulatinglayer 513 (which is shown in FIG. 32). The coils 510 and 512 areconcentric with one another and are provided on one surface of a Macorblock 514 (see FIG. 29) which supports a silicon substrate 515 (FIGS. 28and 29).

A ballast inductor coil 516 is provided in parallel with the coil 510and input leads 517 and 518 are provided for inputting an initialcurrent into the loop formed by the coil 510 and the coil 516. The inputand output leads are separated by a heat switch 519. The function of theheat switch 519 and leads 517 and 518 will be described in detailhereinafter. Suffice it to say for the present description that theleads 517 and 518 and the switch 519 enable an initial current to bestored in the loop formed by the coils 510 and 516 which will bemodulated by movement of the bar 41 during cryogenic operation of thegradiometer to sense changes in the gravitational field.

The coil 516 also provides for tuning of the effective spacing of thecoils 510 and 516 from the surface 512, as will be described in moredetail hereinafter.

The coil 511 is connected parallel to coil 518 which forms part of theSQUID device 367. A fixed ballast inductor in the form of coil 519 canbe provided in parallel with the coils 511 and 518 in order to carry anylarge currents so those currents do not flow into the SQUID device 367.Provided that the inductance of the coil 519 is much greater than thatof the coil 518, the sensitivity is not altered by the inclusion of thefixed ballast inductor 519.

In order to provide a suitable pancake coil for measuring the movementof the surface 512, a large number of turns is required. This makes theformation of conventional coils formed by winding a wire onto asubstrate difficult because of the size of the coil and the restraintson size due to its inclusion in the housing 45 and in proximity to thebars 41 in the gravity gradiometer.

To overcome difficulties of manufacture and expense, the sensing coil isformed from a thin film technology so that the coil is an integratedcircuit formed on a silicon substrate by suitable masking manufacturingtechniques which are well known. However, such thin film technologysuffers from the disadvantage of having relatively low current limitrequirements. To overcome this drawback the circuit is provided with atleast two coils 510 and 511 as described with reference to FIG. 27. Thecoil 511 effectively amplifies the current in the coil 510 suitable forthe SQUID device 367. Thus, the coil 511 effectively forms a transformerto increase the output current of the coil 510. Although this alsodecreases the effective source inductance, this is not a drawbackbecause using high resolution micro-circuits, it is possible to makecoils with many turns and very large inductance.

Thus, as shown in FIG. 29 which is a plan view of the Macor block 514shown in side view in FIG. 28, a silicon substrate 515 is laid on theblock 514 and, as is shown in FIG. 30, a circular aluminium capacitorplate 518 a is then formed on the silicon substrate 515. The plate 518 ais provided with radial slots 519 a to reduce circulation of currentaround the plate 518 a. Concurrently with formation of the capacitorplate 518 a, heater switch input 520 and 521 are formed for supplyingcurrent to the heat switch 519 b. Input and output pads 517 a are alsoformed for supplying the initial source current which flows through thecoil 510 and coil 516. A thin insulating layer 522 is then laid over thecapacitor 518 a, as is shown in FIG. 31. A layer containing the finecoil 510 is then formed on the insulating layer 522, as are input andoutput leads 517 for supplying the initial current which circulatesthrough the loop formed by the coils 510 and 516. The fine coil 510 isformed from superconducting material such as niobium and may have 1200turns, a pitch of 5 microns, an outside diameter of 28 μm and an insidediameter of 16 μm.

An insulating layer is then formed over the coil 510. The insulatinglayer 513 shown in FIG. 32 is then laid over the coil 510 to separatethe coil 510 from the coil 511 and the coarse coil 511 is then laid onthe insulating layer 513 as shown in FIG. 32.

The coarse coil 511 is also made from superconducting material such asniobium and, for example, has 36 turns with a pitch of 150 microns, andoutside and inside diameters which are the same as the fine coil 510.

The ballast coil 516 is provided on the opposite side of the substrate515 to the coils 510 and 511. This is done by providing two substrateswhich are about 0.5 mm thick and gluing the two substrates together sothat the coil 516 is on the outer opposite surface of the formedsubstrate to that on which the coils 510 and 511 are deposited. The coil510 is connected to the coil 516 by bond wires 535 (only one shown inFIG. 28). The Macor block 514 is provided with a slight recess 539 toaccommodate the bond wires 535. Bond wires 536 also extend between thesubstrate 515 and a niobium contact strip 537 formed on the Macor block514.

As is shown in FIG. 33, part of the coarse coil 511 is covered byinsulating strips 530 to enable interconnection of the coil 511 to theSQUID device 367 such as via pads 531 and lead 532 and pad 533, pad 534and lead 535.

In the simplest embodiment of the invention the integrated circuitformed by the aforementioned layers may be as simple as comprising thecoil 510 and the coil 511, as well as the aluminium capacitor plate 518all separated by their respective insulating layers.

In this embodiment the arrangement provides good coupling with K₁₂approaching unity. The initial current circulating in the loop formed bythe coarse coil 511 and the SQUID device 367 can be set to zero with thesensing flux maintained by the current in the coil 510. Although thecurrent is small, the sensing flux is large because the coil 510 has alarge number of turns.

An initial current is stored in the coil 510 (or in the loop formed bythe coil 510 and the coil 516) by supplying a current via input lead 517to the loop. Current is also supplied to the leads 520 and 521 to causethe resistor 519 a to heat up, thereby heating up the part of the loopshown in FIG. 28 adjacent the heating resistor 519 b which underlays thelead 517, as shown in FIG. 32, to heat that part of the lead 517 andtherefore effectively break the superconducting loop. Current suppliedfrom the leads 517 and 518 can then circulate through the loop and thoseleads to induce the initial current in the loop.

Current is then discontinued to the heating resistor 519 b and thecurrent induced in the loop continues to circulate in the loop becauseof the superconducting characteristics of the loop. The current which isinduced in the loop is the current which is modulated by movement of thebar 41 relative to the coil 510 so as to change the magnetic flux whichis produced which in turn alters the current in the coil 511 which inturn is sensed by the SQUID device 367 to provide a measurement of thechange in the gravitational field.

In the embodiment shown in FIGS. 27 and 28 which includes the coil 516,the coil 516, as is previously explained, is mounted on the oppositeside of the substrate 515 to the coil 510 and prevents the bias currentflowing through the coil 510 from flowing in the external leads 517. Thecoil 516 is effectively an exact copy of the coil 510 and is preferablytherefore also formed from a thin film layer deposited onto thesubstrate 515. The bond wires 536 which connect to the strips 537 formthe connections for enabling the coil 511 to be connected to the SQUIDdevice 367.

The coil 516 may also be used to tune the effective spacing of the coil510 from the front face 512 of the bar 41 so that all of the transducerswhich are used can be spaced from the surfaces 512 by the same distance.This will be described in more detail hereinafter, but suffice it to sayfor the present description that coils 516 and 510 can form a singlevirtual coil by suitably selecting the current which is induced in theloop formed by the coils 510 and 516. Thus, by changing that current theposition of the virtual coil effectively moves between the coils 510 and516 to provide a virtual coil position which can be located at apredetermined distance from the face 512. By suitably selecting thecurrents which circulate through the respective loops, tolerances inmanufacture and assembly of the device can be overcome to ensure thatthe virtual coil formed by the coils 510 and 516 are equally spaced fromthe faces 512 of their respective bars.

Thus, the coil 516 can be used to perform the dual function of avoidingbias currents in the external leads as described above, and also tuningof the effective spacing of the coil 510 from the surface 512.

In the embodiments described above, the capacitor plate 518 a isconcentric with the coils 510 and 511. The capacitor plate 518 a doesnot play any part in the operation of the transducer in order to sensechanges in the gravitational field. The capacitor plate 518 a is used tocalibrate the balance of the bars 41 and 42 in their respective houses45 and 47, as will be described in more detail hereinafter. Thepositioning of the capacitor plate 518 a as a concentric arrangementwith the coils 510 and 511 and substantially coplanar with those coilsmeans that the capacitor plate 518 a sees the same signal which is seenby the coil (that is, the gap between the surface 512 and the coil 510).Thus, when the capacitor 518 is used to calibrate the balance of thebars 41 and 42, the capacitor is measuring the same effective signal aswould be seen by the coils during operation of the gradiometer. Thisenables the bars 41 and 42 to be balanced relative to the signal whichis actually detected by the coils 510 during operation of the device,thereby improving the balancing of the bars 41 and 42 and therefore theoperation of the gradiometer.

The plate 518 a is provided concentric with the coils 510 and 511 inthis embodiment by making the plate 518 and the coils 510 and 511 havingsubstantially the same center point. However, in other embodiments theconcentric arrangement can be provided by providing the capacitor plate518 a as separate platelets concentrically arranged about the centerlocation of the coils 510 and 511 rather than a common center, as shownin FIG. 30A. Different geometrical arrangements are also possible.

FIG. 34 shows the location of the block 514 in the opening 305 and thegrooves 402 and is biased by the spring 403 against the shoulders 401 tohold the block 514 in place with the coil 510 being adjacent the edgeface 41 a of the bar 41.

Thus, the coil 510 and the bar 41 form an 1 c circuit so that when thebar 41 moves, the current passing through the coil 510 is changed.

With reference to FIG. 34A and FIG. 34B, a more preferred arrangement ofthe coils 510 and 511 is shown. In the embodiment previously describedthe coils 510 and 511 are generally circular pancake type coils. To moreeasily form the coils and enable interconnection of the coils with othercircuit componentry of the gradiometer, the coils 510 and 511 in FIGS.34A and 34B are meandering coils formed on the block 514 in two separatelayers which are separated by insulation as previously described.

As best shown in FIG. 34A the coarse pitch coil 511 meanders ingenerally curved zigzag fashion and has arms 511 a which are joined bycurved transitions 511 b at respective alternate ends of the arms 511 aas shown in FIG. 34A. The fine pitch coil 510 is not shown in FIG. 34A.However, if the fine pitch coil merely follows the meander of the coil511 so that there are a number of fine pitch meandering arms havingcurrent flowing in opposite directions associated with each arm 511 a,then the current in the arms of the fine pitch coil will simply cancelone another to produce zero net magnetic flux.

The avoid this the fine pitch coil 510 meanders in the manner shown inFIG. 34B relative to the coil 511. The coil 510 has a first arm 510 awhich follows the meandering part of the coil 511 (which is shown indotted lines in FIG. 34B) to the opposite end of the coil 511 a thenreturns along coil section 510 b to form a further arm 510 a′ which thenmeanders in the same manner to return along coil part 510 c to againform a further arm 510 a″. The coil 510 then returns along circuit part510 d to form a still further arm 510 a′″.

Thus, the current flowing through the arms 510 a of the coil 510, whichoverlap the arms 511 a of the coil 511, is in the same direction asindicated by the arrowheads in each of those arms. Therefore, there isno cancelling of the magnetic flux in each coil 510 a associated withthe overlapped arm 511 a of the coil 511. Further still, the coil 510need only cross over itself at one location 512 a as shown in FIG. 34Bin order to provide an output current from the coil 510. The coil part512 a can be on a separate layer to the remainder of the coil 510 (forexample, the same layer as the coarse pitch coil 511) so that theinsulating layer between the coils 510 and 511 separates the circuitpart 512 a from the remainder of the coil 510 shown in FIG. 34B).

The coil 511 is dimensioned such that the width W of the arms 511 a ofthe coarse pitch coil is greater than the space d between the surface ofthe bar 41 and the surface of the block 514 on which the coils 510 and511 are deposited as shown in FIG. 34.

As will be apparent from FIG. 24, four transducers 71 are arrangedadjacent the ends of the bar 41. The other housing 47 also has fourtransducers arranged adjacent the bar 42. Thus, eight transducers 71 areprovided in the gradiometer.

FIG. 35 is a diagram of the bars 41 and 42 showing them in their “inuse” configuration. The transducers which are located in the openings305 are shown by reference numbers 71 a to 71 e to equate to the circuitdiagrams of FIGS. 36 and 37.

With reference to FIGS. 36 and 37, transducers 71 a and 71 b associatedwith the bar 41, and transducers 71 g and 71 e associated with the bar42 are used to provide the gravity gradient measurements.

Input terminals 361 provide input current to the superconductingcircuits shown in FIG. 36. Heat switches which may be in the form ofresistors 362 are provided which are used to initially set thesuperconducting current within the circuit. The heat switches 362 areinitially turned on for a very short period of time to heat those partsof the circuit at which the resistors 362 are located to stop thoseparts of the circuit from superconducting. Currents can then be imposedon the superconducting circuit and when the heat switches formed by theresistors 362 are switched off, the relevant parts of the circuit againbecome superconducting so that the current can circulate through thecircuits subject to any change caused by movement of the bars 41 and 42under the influence of the gravity gradient and angular acceleration, aswill be described hereinafter.

The transducers 71 a, 71 b, 71 g and 71 e are connected in parallel tocircuit line 365 and to circuit line 366 which connect to a SQUID 367.

Thus, as the bars 41 and 42 rotate about their respective flexure web,the bars 41 and 42, for example, come closer to the transducer 71 a andtherefore further away from the transducer 71 b, and closer to thetransducer 71 h and further away from the transducer 71 g respectively.This therefore changes the current flowing through the transducers andthose currents are effectively subtracted to provide signals forproviding a measure of the gravity gradient.

As is shown in FIG. 37, transducers 71 c and 71 d form a separatecircuit and are used for frequency tuning of the bar 41 and transducers71 a and 71 b. Similarly, the transducers 71 e and 71 f are used forfrequency tuning of the bar 42 and the transducers 71 g and 71 h.Frequency tuning of the bars is important because the bars should beidentical in order to reject angular accelerations. The frequency tuningcircuits therefore enable electronic tuning of the bars to matchresonant frequencies and to achieve mode rejection so that each of thebars does function in an identical manner.

The transducers 71 a, 71 b, 71 g and 71 h are also used to form angularaccelerometers for measuring the angular movement of the mounting 5 sothat feedback signals can be provided to compensate for that angularmovement.

To do this, the line 366 is connected to a transformer 370. The polarityof the signals from the transducers 71 a and 71 b and 71 g and 71 h arereversed so that the output of the transducer 370 on lines 371 and 372is an addition of the signals rather than a substraction, as is the casewhen the gradient is measured so the addition of the signals gives ameasure of the angular movement of the bars. The outputs 371 and 372 areconnected to SQUID device 375 for providing a measure of the angularacceleration which can be used in the circuit of FIG. 10 to providecompensation signals to stabilise the mounting 5.

Thus, according to the preferred embodiment of the invention, theangular accelerometers 90′ provide a measurement of angularacceleration, for example, around the x and y axes, and the angularaccelerometer formed by the bars 41 and 42 and the transducers 71 a, 71b, 71 g and 71 h provide a measure of the angular accelerometer aroundthe, for example, z axis.

With reference to FIGS. 38 and 39, the manner in which the balance ofthe bars 41 and 42 is achieved will be described. A pair of displacementsensors formed by capacitors 400 and 401 are provided for two mainpurposes:

-   1. To measure the residual linear acceleration sensitivity of each    bar 41 (and 42) to enable the bars to be mechanically balanced using    the grub screws 301 described with reference to FIG. 24, before    operation at low temperatures; and-   2. To measure the induced linear acceleration sensitivity of each    bar 41 and 42.

The capacitor 400 is formed by the previously described capacitor plate518 a and the surface 41 a of the bar 41. A second circuit the same asthat shown in FIG. 39 is used to measure the change experienced by thecapacitor 401. That circuit is the same as FIG. 38 except the capacitor400 is replaced by the capacitor 401 which is formed by a capacitorplate and surface 41 a relating to another of the transducers 71.

The bars 41 and 42, in their respective housings, are rotated in a jig(not shown) through 360°. This provides an acceleration range of 2g_(E), which is typically 100 times greater than the accelerations whichmay be conveniently applied at low temperature. A typically requirementis for the capacitors 400 and 401 to be able to detect 0.1 nm over aperiod of 1 to 20 minutes. A pair of capacitors 400 and 401 is requiredfor each bar to provide some discrimination against sensor drift, sincerotation of the bar 41 will cause one capacitor 400 to increase and theother capacitor 401 to decrease by the same amount, as is shown in FIG.38, whereas thermal expansion will cause both outputs of the capacitors400 and 401 to increase. The capacitors 400 and 401 remain in place,even though they are unusable at low temperatures, and therefore theircomponents need to be non-magnetic so as to not interfere with theoperation of the gradiometer and, in particular, its nearbysuperconducting circuitry.

FIG. 38 shows that as the bar 41 pivots, the gap applicable to thecapacitor 400 decreases and the gap of the capacitor 401 increases.

The capacitors 400 and 401 are formed by the face 41 a of the bar 41(and the corresponding face on the other bar 42) and second plates 405which are spaced from the face 41 a. The gap between the plates of therespective capacitors 400 and 401 must typically be resolved to about 1ppm.

The capacitor 400 forms a high Q-factor resonant circuit with inductor410. The inductor 410 and capacitor 400 are provided parallel tocapacitors 411 and 412 and connect via capacitor 413 to an amplifier414. The output of the amplifier 414 is provided to a frequency counter415 and also fed back between the capacitors 412 and 411 by line 416.The capacitor 400 therefore determines the operating frequency of theamplifier 414 which can be read to a high precision.

If the bar 41 is out of balance, the frequency counter 45 will tend todrift because of the imbalance of the bar. This can be adjusted bymoving the grub screws 301 into and out of the masses as previouslydescribed until balance takes place. The amplifier 414 can then bedisconnected from the frequency counter 415 so that the gradiometer canbe arranged within the Dewar 1 with the other parts of the circuitsshown in FIG. 39 in place.

FIG. 40 is a detailed view of part of the bar 41 and housing 45 shown inFIG. 24 and marked by the circle A. Because the bar 41 is connected tothe housing 45 by a very thin flexure web 59, if the bar 41 moves toomuch it may exceed the elastic limits of the flexure web 59. This candegrade the flexure joint and therefore the movement of the bar 41 underthe influence of differences in gravitational field experienced at endsof the bar 41.

The amount of movement of the bar 41 which would normally take place andwhich is required in order to provide signals indicative of likelychange in the gravitational field is in the order of 10 microns.Typically the bar 41 is cut from the housing 45 by a wire cuttingoperation which makes a cut such as that labelled 550 in FIG. 40 whichhas a thickness of about 60 microns. Thus, the amount of space which isavailable for the bar 41 to move greatly exceeds that which is requiredand that which may exceed the elastic limit of the flexure web 59. Toprevent the bar 41 from moving beyond the elastic limit (such as morethan plus or minus 10 microns) a cut 551 is made adjacent the end of thebar 41. A similar cut is made at the other end of the bar 41 which isnot shown in FIG. 40. The cut 551 is provided with an enlarged hole 552.The cut 550 which defines the end of the bar 41 is provided with aprofiled section 553 which defines a first abutment surface 554 and asecond abutment surface 555.

The very thin strip of material 556 between cut 551 and the cut 550 hasa profile 557 which matches the profile 553 except that abutmentsurfaces 558 and 559 formed at the end of the profile 557 are spacedapart by a distance of 20 microns less than the space between theabutment surface 554 and 555. Thus, the abutment surfaces 558 and 559can move in the direction of arrow B (as will be explained hereinafter)so that the abutment surfaces 558 and 559 move into the profile 553adjacent to and slightly spaced from the surfaces 554 and 555.

The thin strip of material 506 is moved in the direction of arrow B toso locate the abutment surfaces 558 and 559 by inserting a pin into thehole 552 which pushes the strip of material 556 in the direction ofarrow B so that the surfaces 558 and 559 register with the surfaces 554and 555. Thus, the surfaces 554 and 558 are spaced apart by a distanceof about 10 microns and the surfaces 555 and 559 are spaced apart by adistance of about 10 microns.

Thus, when the bar 41 moves in the direction of double-headed arrow C inFIG. 40 about the flexure web 59, the amount of movement is limited to10 microns because the surface 554 will then engage the surface 558 andthe contact of those surfaces will prevent further movement of the bar41. Similarly, if the bar 41 is moved in the opposite direction, thenthe surface 555 contact the surfaces 559 to again limit the movement toabout 10 microns.

Therefore, movement of the bar 41 is limited to a movement within theelastic limit of the flexure web 59 so the web does not become degradedand adversely influence operation of the gradiometer.

FIGS. 41 and 42 are more detailed drawings showing the connector 5 awhich is used to connect electrical signals from inside the Dewar 1 tocomponentry (not shown) outside the Dewar 1. In particular, thestructure and circuit of FIGS. 41 and 42 is intended to shield the SQUIDdevices 367 from RF interference which may otherwise take place if thereis simply a wire terminal passing through the end plate 4 to theexternal componentry.

The connector 5 a comprises a container 560 which has a bottom wall 561sealed to end plate 4 by an O-ring 562. A lead such as that marked 563passes from inside the Dewar 1 through end plate 4 to a feed throughfilter 564 mounted on the bottom wall 561. A first baffle 567 supports athree terminal cap 565 which is connected to the feed through filter andthe cap 565 is connected to a relay 566 which is supported on a secondbaffle 567. The relay 566 includes a relay switch 568 (see FIG. 42)which in turn passes through a connecting element 570 on the container560 to a lead 571 to connect to the external componentry (not shown).

As is shown in FIG. 41, the lead 563 connects to the feed through filter564 which is comprised of an inductor 571 and a capacitor 572 which isconnected parallel to the inductor 571 on one side and to earth on theother side. The inductor 571 connects to the three terminal cap 565which comprises an inductor 573, an inductor 574 and a capacitor 575.The capacitor 575 is connected parallel to the inductors 573 and 574 onone side and is earthed on the other side. The inductor 574 connects tothe relay 566 which comprises a relay coil 575 and the relay switch 568.When it is desired to conduct signals from the lead 563 to the lead 571,current is supplied to the relay coil 575 to close the switch 568 sothat the signals can pass through the filter 564, the three terminal cap565, the relay switch 568 to the lead 571. The relay being opened whensignals are not conducted cuts off the circuit from the lead 571 to thelead 563 and the three terminal cap 565 and feed through filter 564further shield the SQUID device within the Dewar 1 during operation ofthe gradiometer so as to eliminate RF interference from outside sources,such as television signals and the like, from being conducted throughthe terminal 5 a to the SQUID devices 367.

In other embodiments the capacitors 572 and 575 may be replaced byresistors.

FIG. 42A shows a further part of the RF shielding located in theconnectors 5 b. The wires 563 (only one shown in FIGS. 41 and 42A) eachcomprise twisted wire pairs with each pair being individually screened.Each wire in each pair of wires 563 is connected to inductor 579 a and579 b and two resistors 579 c which are connected in parallel with therespective inductors 579 a and 579 b to provide further RF attenuation.

FIGS. 43 and 44 show the physical configuration and circuit diagram ofone of the measurement bars (i.e. bar 41) and a circuit diagramrespectively which illustrate tuning of the effective spacing of thesensor coil of each transducer with respect to the edge 41 a of the bar41. In the embodiments shown, the transducer 71 b is provided with twocoils 510 and 516 which may be the coils previously described withreference to FIG. 28. The coils 510 and 516 are separated by a space ofabout 1 mm. Heat switch 362 is provided in the loop formed by the coils510 and 516 and the coil 601 of the transducer 71 a at the other end ofthe bar 41. In order to ensure that the coils 601 and 510 are spaced atequal distance from the surfaces 41 a of the bar 41, the current flowingthrough the loop formed by the coils 510, 516 and 601 is proportionedbetween the coils 510 and 516 to form a virtual coil at, for instance,the location D shown in FIG. 44. By changing the proportion of thecurrent which flows through the coils 510 and 516, the position Dchanges between the coils to form an effective virtual coil at thatposition. Thus, if the coils 510 and 601 are not equally spaced fromtheir respective surfaces 41 a, the current induced in the loop can bealtered to in turn alter the amount of current which flows through eachof the coils 510 and 516 to adjust the position D and therefore thevirtual location of a single coil formed from the coils 510 and 516until the spacing matches that of the coil 601.

If desired, the coil 601 could be replaced by a double coil arrangementthe same as that which forms the transducer 71 b shown in FIG. 44. Ofcourse, the transducers 71 a and 71 b can be identical to thosedescribed with reference to FIGS. 27 and 28 in which the coarse coil 511forming a transformer is provided to step up the current which issupplied to the SQUID device 367. For ease of illustration, theadditional coil 511 and the other componentry described with referenceto FIG. 27 through to FIG. 33 is not shown.

As previously explained, the SQUID 367 is initially tuned by inducing acurrent into the loop formed by the coils 510 and 601. This is achievedby supplying current to the heating resistor 362 which forms a heat pumpto elevate the part of the loop at the position of the resistor 362 towarm that part of the circuit above superconducting transition so thatpart of the circuit no longer super-conducts. Thus, a current can besupplied into the loop from, for example, inputs 517 described withreference to FIGS. 27 to 33 and which are not shown in FIG. 44, so thatcurrent circulates through the loop and the current supply connected tothe terminals 517 and 518. The heating resistor 362 is then deactivatedso that the part of the circuit again becomes super-conducting and thecurrent supply is disconnected from the loop so that the current inducedin the loop continues to circulate through the loop undersuper-conducting conditions.

To proportion the current through the coils 510 and 516, a further heatswitch 362′ is provided which enables a current to be induced in theloop formed by the coils 510 and 516 which can travel in the directionof arrow E in FIG. 44. The current induced by the heat switch 362circulates in the direction of arrow F. Therefore, the amount of currentwhich passes through the coil 510 can be altered compared to that whichpasses through the coil 516, thereby shifting the position D of thevirtual coil formed by the coils 510 and 516. Thus, the spacing of thecoils so that the spacing of the coil 510 and the coil 601 are the sameis electronically achieved.

That current is proportionally passed through the coils 510 and 516 toset the virtual position of the coil 510 at position D if necessary, sothat the coils 601 and 501 are effectively spaced from the surfaces 41 aby precisely the same distance. As the bar 41 moves under the influenceof the gravity gradient, the coils 601 and 510 will therefore moverelative to the surfaces 41 a, changing the induced current passingthrough those coils which in turn is sensed by the SQUID device 367 toprovide a measure of the movement and therefore of the gravity gradientexperienced by the bar 41.

The coils 601 and 510 enable angular motion to be distinguished fromlateral motion. Any lateral movement of the bar 41 to the right or leftin FIG. 45 will produce the same effect on both coils, whereas anangular movement under the influence of the gravity gradient will causeone end of the bar 41 to move closer to its corresponding coil and theother end to move further away from its coil.

Whilst the heat switches 362 previously described may take theconventional form of resistors, in one embodiment of the invention theheat switches comprise semi-conducting material such as a Hall effectsensor 570 as shown in FIG. 45. The Hall effect sensor 570 has leads 571and 572 for powering the sensor to in turn elevate the temperature ofpart of the circuit labelled 575 to which it relates, above thesuper-conducting threshold so as to effectively open the circuit at thatpoint so a current can be induced in the circuit from an outside sourceand so when the sensor is turned off and the device returns to cryogenicoperation, the induced current supplied by the outside source simplycontinues to circulate through the circuit under superconductingconditions.

The use of the semi-conductor material and, in particular, the Halleffect sensor has the advantage that it works in the cold environment,is non-magnetic and also is very compact.

Further still, the Hall effect sensor 570 has a further advantage ofbeing non-magnetic and heatable. The non-magnetic characteristicsthereby avoid interference with a super conducting circuitry and theusually undesirable characteristic of heatability of the sensor 570allows the sensor 570 to be used as the switch as previously explained.The sensor 570 also has high resistance in the order of 1K ohm at 4° Kwhich is also advantageous.

FIGS. 45A to 45E show the heat switch 570 and its arrangement in thegradiometer in more detail. With reference to these figures and inparticular FIG. 45A, the bar 41 in the housing 45 is shown along withthe transducers 71. A circuit board 850 is supported by the housing in agroove 861 (see FIG. 45C) and located in place by screws 863 (only oneshown in FIG. 45C). The circuit board 850 supports electronic circuitrysuch as the squid device and the like which are collectively shown bythe block 859 in FIG. 45C. With reference to FIGS. 45A and 45B, as isalso previously explained, the Macor core block 514 on which the coils510 and 511 are deposited has strips 537 on its edge for conductingcurrent to the circuitry 859. As previously explained, the block 514 isbiased into place by spring 403.

The circuit board 850 has a plurality of conducting strips 856 which, inthis embodiment are formed from super conducting material, namelyniobium, which interconnect with the circuitry 859. The strips 537 areconnected to the strips 856 by bridges 852 also formed from niobium. Thebridges 852 are separated from the spring 403 by insulation which may bea varnish coating on the spring 403 or alternatively by suitably spacingthe bridges 852 away from the spring 403.

As is best shown in FIG. 45C the circuit board 850 has a conductingsubstrate such as a copper substrate 865 on its under surface on whichthe Hall effect sensor 570 is located. As best shown in FIG. 45D thesensor 570 has four terminals or connector pins 867. In this embodimentonly two of the pins 867 are used so as to cause a current to flowthrough the sensor 570 from current leads 571 and 572. The leads 571 and572 connect with pads 869 formed from the copper substrate materialwhich is etched at 870 to insulate the pads 867 from the remainder ofthe substrate 865. As shown in FIG. 45E the leads 571 and 572 passthrough the circuit board 850 and fine copper wires 873 may be used tojoin the leads 571 and 572 to the pins 867.

The superconducting circuit 575 wraps around one of the pins 867 so thatwhen current passes through the sensor 570 the sensor is heated and thatheat is conducted to the pin 867 to in turn heat the part of the circuit575 wrapped around the pin 867 to open the circuit 575 as previouslyexplained. The circuit 575 is attached to the copper substrate 865 atlocations 879 in FIG. 45D by varnish or the like so that when the sensor570 is switched off the pin 867 and the circuit 575 quickly coolsbecause heat can be conducted away through the substrate 865. Thus, thecircuit 575 returns to its closed superconducting state.

The preferred embodiment of the heat switch 570 therefore takesadvantage of the usually unwanted characteristic of such devices beingthe heating of the device, as well as the non-magnetic nature and highresistance of the device.

As is shown in FIG. 44, if the transducer 71 a is also formed by adouble coil 601 and 601 a as shown in dotted lines, the current can bemade to circulate only through each loop formed by the respective coils510 and 516, and 601 and 601 a, thereby producing zero current at lead576 to which the SQUID device is connected. Therefore, perturbation ofthe lead microphonics leading to the SQUID device 367 goes away.

In a still further embodiment of the invention, rather than providingone pair of measurement bars formed by the bars 41 and 42, at least oneorthogonal extra pair of bars may be provided. The second pair of barsmay be the same in configuration as the bars 41 and 42 and theirrespective housings 45 and 47 and may be located at the positions of theaccelerometers 90″ shown in FIG. 22. This arrangement is shown in FIG.46. The first pair of bars provided in the housings 45 and 47 which areshown in FIGS. 22 and 46 provide respectively a measure of thedifference between tensor components G_(ZZ) and G_(YY) (G_(ZZ)−G_(YY))and the second pair of bars provided in the housings marked 45′ and 47′in FIG. 46 provide a measure of the difference between the tensorcomponents G_(ZZ) and G_(XX) (G_(ZZ)−G_(XX)).

It should be understood that the subscripts given in the componentsreferred to above are with respect to the X and Y axes being in ahorizontal plane and orthogonal, and a Z axis being a vertical axis. Aspreviously mentioned, the bars 41 and 43 in the housings 45 and 47 areorthogonal with respect to one another and the bars in the housing 45′and 47′ are also orthogonal with respect to one another. The bars 41 and43 are also arranged in spaced apart planes which are orthogonal tospaced apart planes in which the bars of the housings 45′ and 47′ arelocated. It should be further understood that in FIG. 46, thegradiometer is not shown in the orientation it would take up when inuse. When in use the gradiometer is effectively rotated 90° from theposition shown in FIG. 46 so the dotted line in FIG. 46 forms the X axisor direction of flight of the aircraft carrying the gradiometer. Themanner in which the movement of the bars in the housings 45′ and 47′move and provide measurement signals is exactly the same as thatdescribed in the previous embodiments. Typically, when a survey isflown, the aircraft flies across the so-called geological strike of theregion which is being surveyed. The provision of two sets of bars in thegradiometer shown in FIG. 46 results in a single flight simultaneouslymeasuring data from the two sets of measurement bars and therefore hasthe advantage that the data is relevant to the same point along thesurvey lines.

In various embodiments of the invention, the data which is collectedfrom the two sets of survey bars can be manipulated by a processor 800shown in FIG. 46 to provide a measure of one or more than one componentof the gravity gradient tensor. Because the data is received from twosets of measurement bars and is processed, the actual measure of acomponent of the tensor, such as the G_(ZZ) component, can be obtainedfor individual points along a survey line. This therefore enablessurveys to be conducted flying much wider lines than is the case withconventional geological surveys, and therefore the gradiometer of theembodiment of FIG. 46 can be used for both geological surveys andregional surveys with the survey lines being a relatively large distanceapart.

In situations where only two bars are used, a grid of data needs to beobtained in order to enable processing by a mathematical transformtechnique in order to obtain measurements of a single component of thetensor. This generally requires the grid to be produced by flyingrelatively close survey lines and because of the nature of theprocessing, the data is usually presented as a grid of data whichprovides an overall indication of the survey region. Thus, with thepresent embodiment of the invention, data which is collected from theactual point of interest is analysed to produce the component. If onlytwo bars are used, a grid of data is needed and processing by a Fouriertransform technique or the like is required where data from theparticular point plus surrounding points is used to obtain a measure ofthe component. Thus, in order for the measure to be accurate, it isnecessary that the survey lines be close together.

In still further embodiments of the invention a further set ofmeasurement bars could be provided so that six bars are used to providemeasurements to again enable various combinations of components to bemanipulated by the processor to obtain measurements relative to anydesired component of the gravity gradient tensor which may be required.These additional measurements should also allow additional processing toimprove signal to noise.

As previously explained, data from the transducers (not shown in FIG.46) which detect movement of the bars 41 and 43 is supplied to a SQUIDdevice 367. The SQUID device 367 is only schematically shown in FIG. 46for illustration purposes. Data produced by the SQUID device can bemanipulated by processor 800 which can be physically connected to thegradiometer of FIG. 46 but which, more likely than not, is a separateprocessor at a remote location. If the processor 800 is at a remotelocation, data from the SQUID device 367 and other processingcomponentry associated with the gradiometer can be recorded on arecordable medium 900 and loaded into the processor 800 for manipulationor can be forwarded to the processor 800 by a communication link. Theprocessor 800 processes the data obtained from the two sets ofmeasurement bars in the following manner:G _(XX) +G _(YY) +G _(ZZ)=0  (Equation 1)G_(ZZ)−G_(XX)  (Measurement 1)G_(ZZ)−G_(YY)  (Measurement 2)

equation 1 being a known relationship between the components of thegravity gradient tensor given in equation 1;

measurement 1 being the measurement obtained by the first pair of bars;

measurement 2 being the measurement obtained by the second pair of bars;

adding measurements 1 and 2 gives:

$\begin{matrix}\begin{matrix}{{G_{ZZ} - G_{XX} + G_{ZZ} - G_{YY}} = {{2G_{ZZ}} - G_{XX} - G_{YY}}} \\{= {{2G_{ZZ}} - \left( {G_{XX} + G_{YY}} \right)}}\end{matrix} & \left( {{Equation}\mspace{20mu} 2} \right)\end{matrix}$

from equation 1 G_(XX)+G_(YY)=−G_(ZZ) and substituting into equation 2gives:2G_(ZZ)−(−G_(ZZ))=3G_(ZZ)

Since modifications within the spirit and scope of the invention mayreadily be effected by persons skilled within the art, it is to beunderstood that this invention is not limited to the particularembodiment described by way of example hereinabove.

In the claims which follow and in the preceding description of theinvention, except where the context requires otherwise due to expresslanguage or necessary implication, the word “comprise” or variationssuch as “comprises” or “comprising” is used in an inclusive sense, i.e.to specify the presence of the stated features but not to preclude thepresence or addition of further features in various embodiments of theinvention.

1. A gravity gradiometer for measuring components of the gravitygradient tensor, comprising: a sensor for measuring the components ofthe gravity gradient tensor, the sensor including super-conductingcomponentry; a Dewar in which the sensor is arranged; a connector forconnecting the super-conducting componentry within the Dewar to externalequipment outside of the Dewar, the connector comprising: a containerattached to the Dewar; a feed through filter in the container forconnection to a lead within the Dewar; a three terminal cap electricallyconnected to the feed through filter; a relay electrically connected tothe three terminal cap; and an output terminal on the container forconnecting the relay to an external lead, wherein the feed throughfilter comprises an inductor connected in parallel to a load, the otherside of the load being earthed.
 2. The gradiometer of claim 1 whereinthe feed through filter comprises an inductor connected in parallel toone side of a capacitor, the other side of the capacitor being earthed.3. The gradiometer of claim 1 wherein the three terminal cap comprises apair of inductors between which a capacitor is connected on one side,the capacitor being connected to earth on the other side.
 4. Thegradiometer of claim 1 wherein the relay comprises a relay coil, a relayswitch which is closed when the relay coil is energised to enablesignals from the three terminal cap to pass to the terminal.
 5. Thegradiometer of claim 1 wherein a current source is provided forsupplying current to the relay coil when measurements are taken toenergise the coil and close the relay.
 6. The gradiometer of claim 1wherein the three terminal cap is mounted on a first baffle locatedwithin the container and the relay is mounted on a second bafflecontained within the container.
 7. The gradiometer of claim 1 whereinthe gradiometer has a second connector electrically connected to thefirst connector, the second connector having a further RF attenuatorcomprising coils connected in parallel to respective further loads. 8.The gradiometer of claim 7 wherein the further loads comprise resistors.